Tf33-100 (e3a/b/c) Aircraft Engine Parts

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Filter By: Retaining Rings
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Part Number
NSN
NIIN
1-97164A37 Retaining Ring
002635877
10160158 Retaining Ring
005978487
10183828 Retaining Ring
008049734
117507 Retaining Ring
008037304
12Z5010-2 Retaining Ring
005978487
12Z64PC2 Retaining Ring
002635877
196E184-35 Retaining Ring
008037304
197164A37 Retaining Ring
002635877
21003 Retaining Ring
008037304
2186D42 Retaining Ring
008037304
234685 Retaining Ring
002857939
2409-1016557PCP2499-426 Retaining Ring
002635877
277-501-1031 Retaining Ring
005978487
3000-X31-SS2 Retaining Ring
005978487
3000-X43-ST-CD Retaining Ring
008049734
3000-X43-ST-PA Retaining Ring
008049734
3100-156 Retaining Ring
008037304
3100-156-ST-CD Retaining Ring
008037304
3100-66-ST-CD Retaining Ring
002821830
Page:

Engine, Aircraft, Tf33-100 (e3a/b/c)

Picture of Tf33-100 (e3a/b/c)  Aircraft Engine

The Pratt & Whitney JT3D is an early turbofan aircraft engine derived from the Pratt & Whitney JT3C turbojet. It was first run in 1958 and was first flown in 1959 under a B-45 Tornado test aircraft. Over 8,000 JT3Ds were produced between 1959 and 1985. Most JT3D engines still in service today are used on military aircraft, where the engine is referred to by its USAF designation of TF33.

Aware of the competition from the Rolls-Royce Conway turbofan, Pratt&Whitney decided to develop the JT3D turbofan from the JT3C turbojet for later deliveries of the Boeing 707 and the Douglas DC-8, then nearing entry into service. A 2-stage fan replaced the first 3 stages of the 9-stage JT3C LP compressor. On the LP turbine, the second stage was enlarged and a third stage added.

Unlike GE with the CJ805-23, Pratt & Whitney had not undertaken any transonic fan research prior to designing the JT3D, so they were unable to incorporate a single stage unit into the specification. Instead P&W designed a 2-stage unit based on some research they had done to support the J91 nuclear turbojet.

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